材料科学
辅助
复合材料
陶瓷
热导率
保温
极限抗拉强度
各向同性
弹性(材料科学)
压力(语言学)
模数
热的
横截面
陶瓷基复合材料
断裂(地质)
热膨胀
蜂巢
蜂窝结构
变形(气象学)
热传导
航天飞机热防护系统
纳米材料
Timoshenko梁理论
弹性体
气凝胶
抵抗
纳米纤维
分层(地质)
应力-应变曲线
变形机理
弹性模量
热稳定性
梁(结构)
屈曲
作者
方智敏,Shengnan Meng,Cunyi Zhao,Jianyong Yu,Xueli Wang,Yang Si
摘要
ABSTRACT Ceramic aerogels exhibit exceptional thermal insulation potential in extreme environments, yet their poor stretchability and transverse contraction prevent them from providing conformal thermal protection. These limitations render ceramic aerogels inadequate for aircraft evolving toward hypersonic speeds and morphing configurations. This study employs a topology‐guided multiscale structural strategy, fabricating auxetic ceramic nanofiber aerogels, based on theoretical mechanical models of Timoshenko beam theory and Castigliano's theorem. Leveraging a kirigami‐inspired design that integrates reentrant honeycomb structural membranes to resist transverse contraction and isotropic aerogels to block heat leakage, our auxetic aerogels enable outstanding stretchability and tensile‐invariant thermal insulation properties. Specifically, our aerogels achieve an excellent tensile elongation of up to 22% strain with a fracture stress of 31 kPa fracture stress and a Poisson's ratio of −0.49. Moreover, these aerogels also demonstrate excellent fatigue resistance, enduring 500 stretch‐recovery cycles at a 10% strain without any damage. Furthermore, the aerogels possess ultralow thermal conductivity (33.14 mW·m −1 ·K −1 at 20% strain) while maintaining exceptional thermal stability at 1100°C, resisting tensile deformation without transverse contraction. This study shows promising prospects for lightweight, reliable thermal protection in extreme environments.
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